Aerodynamics Question
george kennie
geobet at gis.net
Sun Aug 3 09:41:50 AKDT 2003
You will realize an increase in belly pitch at KE and adverse roll
couple, but you should be able to mix out any ill effects.
Bob Pastorello wrote:
> Given a "typical" pattern design, with stab approx. on
> centerline/thrustline, no engine thrust offsets....lowering the WING
> *chordline* relative to the fuse centerline/thrustline....one would
> expect what undesired trim change?
> Bob Pastorello, Oklahoma
> NSRCA 199, AMA 46373
> rcaerobob at cox.net
> www.rcaerobats.net
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